EP2722721A1 - Steuerungsassistenzverfahren eines Luftfahrzeugs bei der Landung, und Steuerungsassistenzsystem, das in der Lage ist, dieses Verfahren umzusetzen - Google Patents
Steuerungsassistenzverfahren eines Luftfahrzeugs bei der Landung, und Steuerungsassistenzsystem, das in der Lage ist, dieses Verfahren umzusetzen Download PDFInfo
- Publication number
- EP2722721A1 EP2722721A1 EP13189235.8A EP13189235A EP2722721A1 EP 2722721 A1 EP2722721 A1 EP 2722721A1 EP 13189235 A EP13189235 A EP 13189235A EP 2722721 A1 EP2722721 A1 EP 2722721A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- aircraft
- target
- landing
- pilot
- screen
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 19
- 238000013459 approach Methods 0.000 claims description 13
- 230000006870 function Effects 0.000 claims description 8
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 7
- 230000008859 change Effects 0.000 claims description 7
- 230000004048 modification Effects 0.000 claims description 5
- 238000012986 modification Methods 0.000 claims description 5
- 238000010200 validation analysis Methods 0.000 description 15
- 238000004364 calculation method Methods 0.000 description 11
- 239000003550 marker Substances 0.000 description 5
- 238000005259 measurement Methods 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 101150052012 PPP1R14B gene Proteins 0.000 description 2
- 101100013829 Zea mays PHI1 gene Proteins 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000003416 augmentation Effects 0.000 description 1
- 230000003190 augmentative effect Effects 0.000 description 1
- 238000009530 blood pressure measurement Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
- G08G5/025—Navigation or guidance aids
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D2045/008—Devices for detecting or indicating hard landing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
Definitions
- the aircraft For such a landing the aircraft is generally guided automatically, according to its flight plan, to a height called “decision height", and if visibility is sufficient at this decision height, the pilot controls the aircraft manually until landing.
- the present invention relates more particularly to the phase corresponding to the flight of the aircraft between its passage at this decision height and its landing.
- the systems of the aircraft perform its guidance along a predetermined trajectory using either an external relative positioning system (in particular of the ILS type) which provides a trajectory deviation directly, ie absolute position information of the aircraft available on board the aircraft as well as the geographical coordinates of the runway.
- This absolute position of the aircraft can in particular be provided by an inertial unit or by a VOR type system ("Very High Frequency Omnidirectional Range” in English) or GNSS ("Global Navigation Satellite System” type), in particular GPS type ("Global Positioning System” in English) or Galileo.
- GNSS Global Navigation Satellite System
- Such a GNSS system may or may not be augmented by local registration, for example by using a Wide Area Augmentation System (WAAS) network.
- WAAS Wide Area Augmentation System
- the document US5,593,114A describes a landing aid system for an aircraft in which a pilot has means to display a cursor on a screen where an airstrip is also displayed.
- This slider comprises a cruciform symbol corresponding to a desired point of contact of the aircraft with the ground, as well as a line corresponding to a taxiing trajectory of the aircraft.
- the pilot has an interface to adjust the position and orientation of the cursor on the airstrip.
- the system also displays a symbol corresponding to the speed vector of the aircraft. To be able to land on the runway, the pilot must align the symbol representing the speed vector with the cruciform symbol of the cursor. This system therefore helps the pilot during landing by displaying the cursor on which he must align the symbol representing the speed vector.
- the movements of the aircraft during landing have the effect of producing movements of the cursor relative to the airstrip on the screen. This occurs in particular when the pilot is maneuvering the aircraft so as to try to align the symbol representing the velocity vector with the cruciform symbol of the cursor. Therefore, depending on the movements of the aircraft, the pilot is brought, several times during landing, having to change the setting of the position and the cursor orientation by means of said interface. This is an additional workload for the pilot who must continuously monitor the position and orientation of the cursor relative to the runway and modify them if necessary. Moreover, such a mode of operation is not compatible with an automatic landing of the aircraft since the pilot must change the cursor settings several times during landing.
- This method therefore allows a pilot to define a value of the target in superposition of the view from outside the aircraft, then to validate this value.
- the target is positioned on the screen relative to the view from the outside of the aircraft, therefore relative to the landing zone.
- This view from the outside of the aircraft being a view from the current position of the aircraft, the value of the target validated by the pilot is therefore referenced with respect to the current position of the aircraft. Therefore the trajectory determined in step B) allows the aircraft to land in accordance with this target, without being disturbed by the position error of the aircraft when it is at the decision height.
- the trajectory being memorized, it suffices to guide the aircraft along it so as to make a landing in accordance with the value of the target validated by the pilot.
- This memorized trajectory is insensitive to the movements of the aircraft after said validation of a value of the target by the pilot.
- This trajectory extends between the current position of the aircraft during the validation of the target by the pilot in step A3) and the position of the target validated by the pilot.
- the target comprises a ground target point.
- it further comprises an axis of a ground taxiing path and / or the FPA slope ("Flight Path Angle") of the last approach segment of the ground target point.
- the screen is a head-up display device type HUD ("Head Up Display” in English).
- HUD Head Up Display
- the view from the outside of the aircraft corresponds to what the pilot sees, outside the aircraft, when he looks through this HUD type screen. It is therefore not necessary to acquire and display this view using means on board the aircraft.
- the landing zone on the ground corresponds to an airstrip.
- the value of the target displayed in step A1) is determined according to characteristics of the landing runway. These characteristics can in particular correspond to coordinates of the airstrip.
- the value of the target displayed in step A1) is determined according to the current route of the aircraft.
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Traffic Control Systems (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1260036A FR2997066B1 (fr) | 2012-10-22 | 2012-10-22 | Procede d'aide au pilotage d'un aeronef lors d'un atterrissage et systeme d'aide au pilotage apte a mettre en œuvre ce procede |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2722721A1 true EP2722721A1 (de) | 2014-04-23 |
EP2722721B1 EP2722721B1 (de) | 2016-11-30 |
Family
ID=47425135
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13189235.8A Active EP2722721B1 (de) | 2012-10-22 | 2013-10-18 | Steuerungsassistenzverfahren eines Luftfahrzeugs bei der Landung, und Steuerungsassistenzsystem, das in der Lage ist, dieses Verfahren umzusetzen |
Country Status (3)
Country | Link |
---|---|
US (1) | US9377782B2 (de) |
EP (1) | EP2722721B1 (de) |
FR (1) | FR2997066B1 (de) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3110985A1 (fr) * | 2020-05-29 | 2021-12-03 | Airbus | Interface homme-machine d’un aéronef en phase de décollage ou d’atterrissage |
CN114519946A (zh) * | 2022-02-15 | 2022-05-20 | 安胜(天津)飞行模拟系统有限公司 | 一种空中指引显示方法、装置、设备以及存储介质 |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9098999B2 (en) * | 2013-09-13 | 2015-08-04 | The Boeing Company | Systems and methods for assuring the accuracy of a synthetic runway presentation |
US10514707B1 (en) * | 2014-06-26 | 2019-12-24 | Rockwell Collins, Inc. | Flight phase stability indicator system and method |
GB2529684A (en) * | 2014-08-29 | 2016-03-02 | Bae Systems Plc | Image display |
GB2529682A (en) | 2014-08-29 | 2016-03-02 | Bae Systems Plc | Image display |
DE102014014446A1 (de) * | 2014-09-26 | 2016-03-31 | Airbus Defence and Space GmbH | Redundantes Bestimmen von Positionsdaten für ein automatisches Landesystem |
FR3030033B1 (fr) * | 2014-12-15 | 2016-12-16 | Thales Sa | Dispositif d'affichage et de mise a jour d'un motif de trajectoire aerienne en regard d'une zone au sol, notamment pour une mission de largage |
FR3044808B1 (fr) * | 2015-12-03 | 2021-01-15 | Airbus Operations Sas | Procede et systeme d'aide a l'atterrissage d'un aeronef |
FR3044807B1 (fr) * | 2015-12-03 | 2017-11-24 | Airbus Operations Sas | Procede et systeme d'aide a l'atterrissage d'un aeronef |
FR3044809B1 (fr) * | 2015-12-03 | 2017-11-24 | Airbus Operations Sas | Procede et systeme d'aide a l'atterrissage d'un aeronef. |
ES2900737T3 (es) * | 2016-12-21 | 2022-03-18 | Safran Landing Systems Uk Ltd | Montaje de aeronave y método |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5593114A (en) | 1994-04-19 | 1997-01-14 | Mcdonnell Douglas Corporation | Synthetic vision automatic landing system |
FR2752051A1 (fr) * | 1996-08-02 | 1998-02-06 | Sextant Avionique | Dispositif d'assistance au guidage d'un vehicule sur une trajectoire |
FR2896073A1 (fr) * | 2006-01-11 | 2007-07-13 | Airbus France Sas | Systeme de pilotage d'un aeronef, au moins pour piloter l'aeronef lors d'une approche autonome en vue d'un atterrissage. |
WO2009042309A2 (en) * | 2007-08-17 | 2009-04-02 | Sikorsky Aircraft Corporation | Stabilized approach to a point in degraded visual environment |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8010245B2 (en) * | 2008-09-30 | 2011-08-30 | Honeywell International Inc. | Aircraft systems and methods for displaying a touchdown point |
US8589071B2 (en) * | 2011-08-15 | 2013-11-19 | Honeywell International Inc. | Aircraft vision system including a runway position indicator |
-
2012
- 2012-10-22 FR FR1260036A patent/FR2997066B1/fr not_active Expired - Fee Related
-
2013
- 2013-10-18 EP EP13189235.8A patent/EP2722721B1/de active Active
- 2013-10-21 US US14/058,690 patent/US9377782B2/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5593114A (en) | 1994-04-19 | 1997-01-14 | Mcdonnell Douglas Corporation | Synthetic vision automatic landing system |
FR2752051A1 (fr) * | 1996-08-02 | 1998-02-06 | Sextant Avionique | Dispositif d'assistance au guidage d'un vehicule sur une trajectoire |
FR2896073A1 (fr) * | 2006-01-11 | 2007-07-13 | Airbus France Sas | Systeme de pilotage d'un aeronef, au moins pour piloter l'aeronef lors d'une approche autonome en vue d'un atterrissage. |
WO2009042309A2 (en) * | 2007-08-17 | 2009-04-02 | Sikorsky Aircraft Corporation | Stabilized approach to a point in degraded visual environment |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3110985A1 (fr) * | 2020-05-29 | 2021-12-03 | Airbus | Interface homme-machine d’un aéronef en phase de décollage ou d’atterrissage |
US11639235B2 (en) | 2020-05-29 | 2023-05-02 | Airbus (S.A.S.) | Human-machine interface of an aircraft in take-off or landing phase |
CN114519946A (zh) * | 2022-02-15 | 2022-05-20 | 安胜(天津)飞行模拟系统有限公司 | 一种空中指引显示方法、装置、设备以及存储介质 |
CN114519946B (zh) * | 2022-02-15 | 2023-09-12 | 安胜(天津)飞行模拟系统有限公司 | 一种空中指引显示方法、装置、设备以及存储介质 |
Also Published As
Publication number | Publication date |
---|---|
US20140114506A1 (en) | 2014-04-24 |
US9377782B2 (en) | 2016-06-28 |
FR2997066A1 (fr) | 2014-04-25 |
FR2997066B1 (fr) | 2016-01-29 |
EP2722721B1 (de) | 2016-11-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2722721B1 (de) | Steuerungsassistenzverfahren eines Luftfahrzeugs bei der Landung, und Steuerungsassistenzsystem, das in der Lage ist, dieses Verfahren umzusetzen | |
EP1614086B1 (de) | Sicheres interaktives 3d-navigationsverfahren und einrichtung | |
EP1891618B1 (de) | Verfahren und system zur hilfe bei der flugkontrolle eines tieffliegenden flugzeugs | |
EP0916073B1 (de) | Hilfsvorrichtung zur lenkung eines fahrzeugs entlang einer trajektorie | |
FR3009117A1 (fr) | Procede et systeme d'atterrissage automatique autonome | |
EP2600330B1 (de) | System und Verfahren zur Ausrichtung von Flugzeug- und Landebahnrichtungen während des Rollens beim Start | |
EP1464576B1 (de) | Verfahren und Einrichtung zur Steuerungshilfe eines Flugzeugs während der Landung | |
EP1999435B1 (de) | Flugzeugleitsystem | |
EP1987503A1 (de) | Vorrichtung zur unterstützung der flugzeuglenkung in der landeanflugsphase zum landen | |
FR2896071A1 (fr) | Procede et dispositif d'aide au pilotage d'un aeronef lors d'une approche autonome. | |
EP0722132B1 (de) | Verfahren zur Steuerung eines Flugzeuges durch das Folgen auf einer, mittels Passierpunkten bestimmten horizontalen Flugbahn | |
EP1971973A2 (de) | System zur steuerung eines flugzeuges | |
FR2847553A1 (fr) | Dispositif d'aide a l'interception par un aeronef d'un segment d'une trajectoire situee dans un plan horizontal et systeme d'aide a l'interception et au suivi d'un tel segment | |
FR2949897A1 (fr) | Procede d'assistance au pilotage d'un aeronef et dispositif correspondant. | |
FR2783500A1 (fr) | Dispositif d'aide au pilotage d'un aeronef, notamment a voilure tournante et en particulier un helicoptere | |
FR2990527A1 (fr) | Procede et dispositif d'aide a la gestion du vol d'un aeronef lors d'une phase d'atterrissage. | |
FR2904706A1 (fr) | Procede et dispositif pour determiner une hauteur de decision lors d'une approche autonome d'un aeronef. | |
EP3216021A1 (de) | Verfahren und vorrichtung zum lenken eines flugzeugs | |
CA2160759C (fr) | Dispositif optoelectronique d'aide au pilotage d'un aeronef | |
US7584027B2 (en) | Aircraft navigation aid method and corresponding device | |
FR3017703A1 (fr) | Procede et systeme de determination de la compatibilite d'un guidage angulaire avec une approche | |
CA2460605C (fr) | Procede et dispositif pour determiner au moins une information de position verticale d'un aeronef | |
WO2021228923A1 (fr) | Dispositif électronique, et procédé, de guidage du pilote dans le pilotage d'un aéronef lors de l'atterrissage en présence de vent de travers | |
FR3089955A1 (fr) | Procede et systeme de guidage d’aide au suivi d’une trajectoire pour un pilotage au vecteur-vitesse d’un aeronef | |
WO2017194847A1 (fr) | Pilotage automatique d'un aéronef à déconnexion différée |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
17P | Request for examination filed |
Effective date: 20141023 |
|
RBV | Designated contracting states (corrected) |
Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
INTG | Intention to grant announced |
Effective date: 20160817 |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: PERRIN, FABIEN Inventor name: EBERLE, MATTHIAS Inventor name: PUYOU, GUILHEM Inventor name: BARBA, MATTHIEU |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 850371 Country of ref document: AT Kind code of ref document: T Effective date: 20161215 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: FRENCH |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602013014659 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20161130 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK05 Ref document number: 850371 Country of ref document: AT Kind code of ref document: T Effective date: 20161130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170228 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170301 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170330 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 Ref country code: AT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170228 Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602013014659 Country of ref document: DE |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 5 |
|
26N | No opposition filed |
Effective date: 20170831 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171031 Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171018 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171031 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20171031 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171031 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 6 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171018 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20131018 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20161130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161130 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170330 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R079 Ref document number: 602013014659 Country of ref document: DE Free format text: PREVIOUS MAIN CLASS: G05D0001060000 Ipc: G05D0001485000 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20231020 Year of fee payment: 11 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20231025 Year of fee payment: 11 Ref country code: DE Payment date: 20231020 Year of fee payment: 11 |